Direct noise computation of trailing edge noise at high Reynolds numbers

14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference)

Volumn , Issue , 2008, Pages

  Le Garrec, Thomas ^a   Gloerfelt, Xavier ^a   Corre, Christophe ^b  

^a DYNFLUID LABORATORY   (France)

^b LEGI   (France)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; ANGLE OF ATTACK; BOUNDARY LAYERS; COMPUTATIONAL AEROACOUSTICS; NASA; NUMERICAL METHODS; REYNOLDS NUMBER;

BOUNDARY LAYER TURBULENCE; COMPUTATIONAL AEROACOUSTICS (CAA); EXPERIMENTAL DATABASE; HIGH REYNOLDS NUMBER; HIGH-ORDER NUMERICAL METHOD; LOCAL GRID REFINEMENT; MODERATE REYNOLDS NUMBERS; SEPARATED BOUNDARY LAYERS;

ACOUSTIC NOISE;

EID: 78249253996     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-2914     Document Type: Conference Paper

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